The velocity of air entering in a rocket is ___ as compared to an aircraft. Same Zero Less More TRUE ANSWER : ? YOUR ANSWER : ?
The maximum combustion pressure in gas turbine as compared to I.C. engine is More Less Same Depends on other factors TRUE ANSWER : ? YOUR ANSWER : ?
Separators are generally used in air compressor installations Between the after-cooler and receiver Before first stage suction Before the inter-cooler After the inter-cooler TRUE ANSWER : ? YOUR ANSWER : ?
Reheating in a multistage expansion gas turbine ________ compressor work. Decreases Has no effect on Increases None of these TRUE ANSWER : ? YOUR ANSWER : ?
Gas turbines for power generation are normally used In emergency To supply base load requirements To enable start thermal power plant To supply peak load requirements TRUE ANSWER : ? YOUR ANSWER : ?
Separators in compressor installations are located After receiver After inter-cooler Between after-cooler and air receiver Before inter-cooler TRUE ANSWER : ? YOUR ANSWER : ?
For speed above 3000 km/hour, it is more advantageous to use Rockets Ramjet engine Turbojet engine Propellers TRUE ANSWER : ? YOUR ANSWER : ?
The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio) 1 - (1/r) ɣ-1/ɣ r ɣ-1 1 - (1/r) ɣ/ɣ-1 1 - r ɣ-1 TRUE ANSWER : ? YOUR ANSWER : ?
Gas turbine works on Brayton or Atkinson cycle Carnot cycle Rankine cycle Ericsson cycle TRUE ANSWER : ? YOUR ANSWER : ?
The efficiency of the vane blower is (where W₁ = Workdone due to compression, and W₂ = Workdone due to back flow) (W₁ + W₂)/W₁ W₂/(W₁ + W₂) (W₁ + W₂)/W₂ W₁/(W₁ + W₂) TRUE ANSWER : ? YOUR ANSWER : ?